THE continuing development of aircraft operational concepts has in recent years resulted in the emergence of a variety of flight control functions which are essential to the safety of the aircraft and which moreover have to be performed automatically, the task being either too difficult for the human pilot, or at least so difficult as to command so much of his attention that his ability to carry out other functions is impaired. Among these functions may be instanced automatic landing, autostabilisation of V.T.O.L. aircraft in the hovering flight mode, the autostabilisation of an aircraft in some part of the flight regime in which its own natural stability is negative, and the autopiloting of aircraft operating at extremely low relative altitudes, to avoid collision with the terrain.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A New Development in Multiplex Electro-hydraulic Actuators


    Untertitel :

    A detailed exposition of the design philosophy which has led to the development of a new multiplex actuator


    Beteiligte:
    Maltby, P.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966-12-01


    Format / Umfang :

    10 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Development of Tilt Control System Using Electro-Hydraulic Actuators

    Enomoto, M. / Kamoshita, S. / Kamiyama, M. et al. | British Library Online Contents | 2005



    Electro‐mechanical Actuators

    Maré, Jean‐Charles | Wiley | 2017


    Electro hydrostatic actuators

    LESAGE EMMANUEL / GRAND SERGE | Europäisches Patentamt | 2020

    Freier Zugriff

    Electro‐hydrostatic Actuators

    Maré, Jean‐Charles | Wiley | 2017